Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
THE APPROXIMATION OF THE STANDARD ATMOSPHERE MODEL
RÉSUMÉ
A model of atmospheric density dependence on altitude, convenient for fulfillment of the mathematical simulation of space vehicle entry into Earth's atmosphere, is proposed. Discussed are questions concerning the possibility of replacing this model with a simplified exponential model.
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Yaroshevsky, V. A., The Atmospheric Entry of Different Space Vehicles.
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Bobylev, A. V., Dyadkin, A. A., Kobzev, V. I., Poedinok, V. M., Reshetin, A. G., Suprunenko, S. N., and Yaroshevsky, V. A., Problems of control of re-entry vehicles with a moderate lift-to-drag ratio at atmospheric entry.
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Kopnin, Yu. M., Spatial motion equations of satellites, Using aerodynamic lift.
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Yaroshevsky, V. A., An approximate calculation of the required and disposable cross range realized at vehicle reentry at a given point of the Earth's surface.
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Bobylev, A. V. and Yaroshevsky, V. A., Analytical estimation of the maximum g-factor achieved at the vehicle atmospheric entry.